Aerial vehicle with a controllable gripping device
Patent Information
- Application Number
- TW115202982
- Authority / Receiving Office
- TW · TW
- Patent Type
- Utility models
- Current Assignee / Owner
- Filing Date
- 2026-04-07
- Publication Date
- 2026-09-01
- Estimated Expiration
- 2036-04-06
Smart Images
Figure TWG2TB001909361_001 
Figure TWG2TB001909361_002 
Figure TWG2TB001909361_003
Abstract
Claims
1. An aircraft equipped with a controllable clamping device, comprising: A drive assembly comprising a main body and a plurality of propellers for driving the aircraft; A protective cover encloses the drive assembly and has a notch at the bottom of the protective cover; a clamping device is disposed below the main body and performs a gripping action through the notch; and a control circuit is electrically coupled to the drive assembly and the clamping device to control the operation of the drive assembly and the clamping device; wherein the clamping device is driven by a clamping drive motor and the clamping drive motor is controlled by the control circuit.
2. The aircraft with a controllable clamping device as described in claim 1, wherein the control circuit includes a first microcontroller, a sensing device and a clamping control module electrically connected to the first microcontroller to control the operation of the drive assembly and the clamping device.
3. An aircraft equipped with a controllable clamping device as described in claim 2, wherein the sensing device includes at least an inertial measurement unit and a barometer to maintain the stability of the aircraft's flight attitude.
4. An aircraft with a controllable clamping device as described in claim 3, wherein the sensing device further includes a magnetometer electrically connected to the first microcontroller for sensing the Earth's magnetic field.
5. An aircraft with a controllable clamping device as described in claim 1, wherein the main body is located at the geometric center of a spherical structure and the clamping device is located on the central axis of the aircraft.
6. The aircraft equipped with a controllable clamping device as described in claim 2 further includes a remote controller communicatively connected to the aircraft and used to control the operation of the aircraft, wherein the remote controller includes: a second microcontroller; a control interface including a joystick control module and at least one function key, which respectively generate flight control data and a clamping device operation command; and a second wireless communication module for transmitting the flight control data and the clamping device operation command to the aircraft.
7. The aircraft equipped with a controllable clamping device as described in claim 6 further includes a first wireless communication module for receiving wireless control signals from the remote controller, so that the first microcontroller can synchronously adjust the flight attitude correction and control the action of the clamping device.
8. An aircraft with a controllable clamping device as described in claim 6, wherein the remote controller includes an LED display interface, and the second microcontroller controls the LED display interface to display a corresponding light pattern according to the clamping or releasing state of the clamping device.
9. The aircraft with a controllable clamping device as described in claim 2 further includes a motor control module electrically connected to the first microcontroller, wherein the motor control module includes a plurality of motor control units, each driving a corresponding plurality of motors to individually control the rotational speed of the plurality of propellers.
10. The aircraft with a controllable clamping device as described in claim 2 further includes a battery and a first voltage regulator, the first voltage regulator outputting the voltage of the battery to the first microcontroller and the sensing device at a constant voltage.